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BS EN 16603-20:2023

BS EN 16603-20:2023

$215.11

Space engineering. Electrical and electronic

Published By Publication Date Number of Pages
BSI 2023 138
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PDF Catalog

PDF Pages PDF Title
2 undefined
9 1 Scope
10 2 Normative references
11 3 Terms, definitions and abbreviated terms
3.1 Terms from other standards
3.2 Terms specific to the present standard
18 3.3 Abbreviated terms
20 3.4 Nomenclature
21 4 General requirements
4.1 Interface requirements
4.1.1 Overview
4.1.2 Signals interfaces
4.1.3 Commands
23 4.1.4 Telemetry
4.2 Design
4.2.1 Failure containment and redundancy
4.2.1.1 General requirements
26 4.2.1.2 Reliable insulation
32 4.2.2 Data processing
4.2.2.1 Overview
33 4.2.2.2 Provisions
34 4.2.3 Electrical connectors
35 4.2.4 Testing
36 4.2.5 Mechanical: Wired electrical connections
4.2.6 Miscellaneous
37 4.3 Verification
4.3.1 Provisions
4.3.2 Documentation
38 5 Electrical power
5.1 Functional description
5.2 Power subsystem and budgets
5.2.1 General
5.2.2 Provisions
5.2.2.1 Power subsystem
5.2.2.2 Engineering process
39 5.3 Failure containment and redundancy
40 5.4 Electrical power interfaces
41 5.5 Power generation
5.5.1 Solar cell, coverglass, SCA and PVA qualification
5.5.2 Solar array specification and design
44 5.5.3 Solar array power computation
46 5.5.4 Solar array drive mechanisms
5.6 Electrochemical Energy Storage
5.6.1 Applicability
47 5.6.2 Batteries
49 5.6.3 Battery cell
5.6.4 Battery use and storage
50 5.6.5 Battery safety
5.6.5.1 Overview
5.6.5.2 Provisions
51 5.7 Power conditioning and control
5.7.1 Applicability
5.7.2 Spacecraft bus
55 5.7.3 Battery Charge and Discharge Management
5.7.4 Bus under-voltage or over-voltage
56 5.7.5 Power converters and regulators
57 5.7.6 Payload interaction
58 5.8 Power distribution and protection
5.8.1 General
61 5.8.2 Harness
62 5.9 Safety
5.10 High voltage engineering
63 5.11 Verification
5.11.1 Provisions
5.11.2 <>
64 6 Electromagnetic compatibility (EMC)
6.1 Overview
6.2 Policy
6.2.1 Overall EMC programme
6.2.2 EMC control plan
65 6.2.3 Electromagnetic compatibility advisory board (EMCAB)
6.3 System level
6.3.1 Electromagnetic interference safety margin (EMISM)
6.3.1.1 Circuits categories
66 6.3.1.2 Critical points
6.3.1.3 Margins
6.3.2 Inter-element EMC and EMC with environment
6.3.2.1 Overview
6.3.2.2 EMC with the launch system
6.3.2.3 Protected frequency bands
6.3.2.4 Lightning
6.3.3 Hazards of electromagnetic radiation
67 6.3.4 Spacecraft charging protection program
6.3.4.1 Applicability
6.3.4.2 General
6.3.4.3 Performance
68 6.3.5 Intrasystem EMC
6.3.6 Radio frequency compatibility
6.3.7 Spacecraft DC magnetic field emission
6.3.7.1 Overview
6.3.7.2 Spacecraft with susceptible payload
69 6.3.7.3 Attitude control subsystem
6.3.8 Design provisions for EMC control
6.3.8.1 Electrical bonding
6.3.8.2 Grounding
6.3.8.3 Wiring
6.3.9 Detailed design requirements
6.4 Verification
6.4.1 Verification plan and report
70 6.4.2 Safety margin demonstration for critical or EED circuit
6.4.3 Detailed verification requirements
71 7 Radio frequency systems
7.1 Functional description
72 7.2 Antennas
7.2.1 General
7.2.1.1 Overview
7.2.1.2 Provisions
7.2.1.3 Failure containment and redundancy
73 7.2.2 Antenna structure
7.2.2.1 General
7.2.2.2 Categories
74 7.2.2.3 Elements
77 7.2.2.4 Technologies
78 7.2.2.5 Performance parameters
7.2.3 Antenna interfaces
7.2.3.1 Guided-wave interfaces
79 7.2.3.2 Radiative interfaces
7.2.4 Antennas Verification
7.3 RF Power
7.3.1 Overview
80 7.3.2 RF Power handling (thermal)
7.3.2.1 General requirements
7.3.2.2 Design and Verification
7.3.3 Corona or Gas Discharge
7.3.3.1 General requirements
7.3.3.2 Design and Verification
81 7.3.4 Qualification for power handling and gas discharge
7.4 Passive intermodulation
7.4.1 Overview
7.4.2 General requirements
7.4.3 Identification of potentially critical intermodulation products
82 7.4.4 Verification
7.4.5 Qualification for passive intermodulation
7.5 Verification
83 8 Pre-tailoring matrix per space product and feature types
8.1 Introduction
84 8.2 Use of the inclusive and exclusive requirement categories

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BS EN 16603-20:2023
$215.11